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Brockenbrough_Ch05.qxd  9/29/05  5:12 PM  Page 5.14



                                                 CRITERIA FOR BUILDING DESIGN


                   5.14  CHAPTER FIVE

                                 For singly symmetric members where y is the axis of symmetry,

                                                           F +  F    4 FF H 
                                                                          ey ez
                                                     F =    ey 2 H  ez   1 − 1 −  ( F +  F ) 2      (5.26)
                                                                
                                                      e
                                                                 
                                                                 
                                                                         ey
                                                                             ez
                                 For unsymmetric members, F e is the lowest root of the cubic equation,
                                                                         x   2        y   2
                                                             −
                                         (F −  F ex )(F −  F ey )(F −  F ez ) F e 2 (F −  F ey )    r   − FF −  F ex )    r   = 0  (5.27)
                                                                                        o
                                                                         o
                                                                               2
                                                                               (
                                                 e
                                                                              e
                                          e
                                                                                 e
                                                        e
                                                                  e
                                                                         o
                                                                                        o
                               The following definitions apply:
                                 K z = effective length factor for torsional buckling
                                 G = shear modulus of elasticity of steel = 11,200 ksi (77,200 MPa)
                                                         6
                                                    6
                                 C w = warping constant, in (mm )
                                                        4
                                                   4
                                 J = torsional constant, in (mm )
                                                                        4
                                                                            4
                                 I x , I y = moment of inertia about the principal axes, in (mm )
                                 x o , y o = coordinates of shear center with respect to the centroid, in (mm)
                                  r o  = Polar radius of gyration about shear center, in (mm)
                                                                     I +  I
                                                          r =  x +  y +  x  y                      (5.28)
                                                           2
                                                                  2
                                                               2
                                                           o   o  o
                                                                       A
                                                                x +  y 2
                                                                 2
                                                           H =−  o   o                             (5.29)
                                                              1
                                                                  r o 2
                                                                π  2 E
                                                          F =                                      (5.30)
                                                           ex
                                                              ( KL r / ) 2
                                                                   x
                                                                x
                                                                π 2 E
                                                          F =                                      (5.31)
                                                           ey
                                                              ( KL r / ) 2
                                                                   y
                                                                y
                                                              π 2 EC    1
                                                          F =     w  +  GJ                       (5.32)
                                                           ez
                                                               ( KL) 2    Ar o 2
                                                                 z
                                                                                           2
                               For doubly symmetric I-shaped sections, C w may be taken conservatively as I y d /4. For tees and
                               double angles, take C w and x o as 0.
                   5.4.3 Compressive Strength of Single-Angle Members
                               The compressive strength of single-angle members can be determined from Eqs. (5.19)–(5.21), using
                               KL/r as given in this article and neglecting eccentricity, provided the angles are (1) loaded at the ends
                               in compression through the same one leg, (2) attached by welding or by two-bolt-minimum connec-
                               tions, and (3) subjected to no intermediate transverse loads. For other conditions, see the AISC
                               Specification. The modified slenderness ratios are intended to account indirectly for bending due to
                               eccentricity of loading and end restraint from truss chords.
                                 For equal-leg angles, or unequal-leg angles connected through the longer leg, which are individ-
                               ual members or are web members of planar trusses with adjacent web members attached to the same
                               side of the gusset plate or chord:
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